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High speed, low cost, LEO-thermal-cycling facilityThe design and operations of a low cost, high rate thermal cycling facility designed for LEO conditions is described. Thermal cycling facilities were constructed with various design criteria. Some were designed to duplicate as closely as possible the conditions a cell or module would encounter while in orbit about the Earth. A typical facility to perform this type of cycling was a large vacuum system with liquid nitrogen cooled walls. The cells were heated by an AMO spectrum solar simulator, then a shutter was closed allowing the cells to give up their heat to the cold walls. This system was good at duplicating the orbital conditions but was slow and very costly to operate. Other systems used a gas atmosphere and heated the cells with radiant heat and cooled the cells by moving them into close proximity to a cold plate. The systems greatly increased the cycle times. Other systems moved the heating and cooling atmosphere into and out of the test areas and achieved reasonable cycle rates. All these systems, however, are expensive to operate.
Document ID
19840021271
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hart, R. E., Jr.
(NASA Lewis Research Center Cleveland, OH, United States)
Sidorak, L. G.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Publication Information
Publication: Space Photovoltaic Res. and Technol. 1983
Subject Category
Energy Production And Conversion
Accession Number
84N29340
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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